View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 62923U 26144.95465924 +.00000000 +00000-0 +79988-3 0 00000
2 62923 43.0021 58.3694 0001342 230.3447 129.7287 15.27598251 03
| Epoch (UTC): | 24 May 2026 22:54:42 |
| Eccentricity: | 0.0001342 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.3694° |
| argument of perigee: | 230.3447° |
| revolutions per day: | 15.27598251 |
| mean anomaly at epoch: | 129.7287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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